Single-fitting, dual-circuit fuel nozzle

Patent metadata

Field	Value
Publication number	US-10240793-B2
Application number	US-201414900935-A
Country	US
Kind code	B2
Filing date	Apr 22, 2014
Priority date	Jul 1, 2013
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

A manifold fitting receiving radial and axial manifolds and providing two radial outlets is disclosed. The manifold fitting, when used in conjunction with a fuel injector and a combustor for a gas turbine engine, reduces the radial footprint of the fuel injector and thereby allows for a more compact engine. Additionally, the manifold fitting eliminates parts, reducing weight in the process, as compared to prior art fittings. Such reductions in size, parts count, and weight are particularly beneficial for aircraft applications.

First claim

What is claimed is:

1. A manifold fitting assembly, comprising:
a tube;
a sleeve surrounding the tube, the sleeve and the tube extending along a longitudinal centerline of the manifold fitting assembly and forming a first sleeve cavity therebetween;
a first manifold intersecting the manifold fitting assembly radial to the longitudinal centerline and in fluid communication with the first sleeve cavity, wherein the first manifold extends circumferentially about the longitudinal centerline;
a second manifold intersecting the manifold fitting assembly co-axial with the longitudinal centerline and in fluid communication with the tube;
a first outlet radial to the longitudinal centerline and in fluid communication with the first sleeve cavity;
a second outlet radial to the longitudinal centerline and in fluid communication with the tube;
wherein the tube defines a chamber in fluid communication with the second manifold and the second outlet, and the tube further defines a tube cavity in fluid communication with the first sleeve cavity and the first outlet; and
wherein the sleeve and the tube are connected by an abutment, the abutment forming a second sleeve cavity between the tube and the sleeve, and the second sleeve cavity communicating between the chamber and the second outlet.

2. The manifold fitting assembly of claim 1 , further comprising a first manifold fitting circumscribing the second manifold and defining a first manifold cavity therebetween, the first manifold cavity being in fluid communication with the first sleeve cavity, and the first manifold intersecting and communicating through the first manifold fitting to the first manifold cavity.

3. The manifold fitting assembly of claim 2 , wherein the first manifold fitting is sealed with the sleeve and the second manifold is sealed with the tube.

4. The manifold fitting assembly of claim 3 , wherein a first o-ring seals the first manifold fitting with the sleeve and a second o-ring seals the second manifold with the tube.

5. The manifold fitting assembly of claim 2 , wherein a ferrule surrounds and seals a joint between the first manifold fitting and the sleeve.

6. The manifold fitting assembly of claim 1 , further comprising a fluid filter positioned inside of the tube.

7. The manifold fitting assembly of claim 1 , further comprising a fluid filter positioned in the first sleeve cavity.

8. The manifold fitting assembly of claim 1 , further comprising a flow limiter positioned inside of the tube.

9. A manifold fitting assembly, comprising:
a tube;
a sleeve surrounding the tube and forming a first sleeve cavity therebetween, the first sleeve cavity being in fluid communication with a first outlet, and the tube being in fluid communication with a second outlet;
a second manifold coaxial, and in fluid communication, with the tube;
a first manifold fitting circumscribing the second manifold and defining a first manifold cavity therebetween, the first manifold cavity being in fluid communication with the first sleeve cavity;
a first manifold radially extending from the first manifold fitting and being in fluid communication with the first manifold cavity, wherein the first manifold extends circumferentially about a longitudinal centerline of the manifold fitting assembly;
wherein the tube defines a chamber in fluid communication with the second manifold and the second outlet, and the tube further defines a tube cavity in fluid communication with the first sleeve cavity and the first outlet; and
wherein the sleeve and the tube are connected by an abutment, the abutment forming a second sleeve cavity between the tube and the sleeve, and the second sleeve cavity communicating between the chamber of the tube and the second outlet.

10. The manifold fitting assembly of claim 9 , wherein a ferrule surrounds and seals a joint between the first manifold fitting and the sleeve.

11. The manifold fitting assembly of claim 9 , wherein the first manifold is sealed with the sleeve and the second manifold is sealed with the tube.

12. The manifold fitting assembly of claim 11 , wherein a first o-ring seals the first manifold with the sleeve and a second o-ring seals the second manifold with the tube.

13. A fuel injector of a combustor, the fuel injector comprising:
a fuel nozzle extending into the combustor;
a stem extending away from the fuel nozzle;
a manifold fitting assembly extending from the stem and having a longitudinal centerline extending in a non-radial direction with respect to the combustor, the manifold fitting assembly including a tube and a sleeve circumscribing the tube to define a first sleeve cavity therebetween;
a first manifold intersecting the manifold fitting assembly radial to the longitudinal centerline and in fluid communication with the first sleeve cavity, wherein the first manifold extends circumferentially about the longitudinal centerline;
a second manifold intersecting the manifold fitting assembly co-axial, and in fluid communication, with the tube;
a first outlet radial to the longitudinal centerline and in fluid communication with the first sleeve cavity;
a second outlet radial to the longitudinal centerline and in fluid communication with the tube;
wherein the tube defines a chamber in fluid communication with the second manifold and the second outlet, and the tube further defines a tube cavity in fluid communication with the first sleeve cavity and the first outlet; and
wherein the sleeve and the tube are connected by an abutment, the abutment forming a second sleeve cavity between the tube and the sleeve, and the second sleeve cavity communicating between the chamber and the second outlet.

14. The fuel injector of claim 13 , wherein each manifold is in communication with a separate fuel supply.

15. The fuel injector of claim 13 , further comprising a first manifold fitting circumscribing the second manifold and defining a first manifold cavity therebetween, the first manifold cavity being in fluid communication with the first sleeve cavity, and the first manifold intersecting and communicating through the first manifold fitting to the first manifold cavity.

Assignees

• United Technologies Corp

Inventors

• Low Kevin Joseph

Classifications

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F02C7/22

  Fuel supply systems · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• F02C7/222

  Fuel flow conduits, e.g. manifolds · CPC title